In: Other
Data Provided in the problem statement
CH4 = 80. 62 %
C2H6 = 5.41%
C3H8 = 1. 87%
C4H10 = 1. 60%
N2 = 10. 50%
Burning of fuel reaction takes the form
[ (0. 8062 CH4 + 0. 0541 C2H6 + 0. 0187 C3H8 + 0. 0160 C4H10 + 0. 1050 N2 ] + a ( O2 + 3. 76 N2) ==>
b (0. 078 C02 + 0. 002 C0 + 0. 07 O2 + 0. 85 N2) + c H2O
Here
a =Number of moles of air required
b = moles of products formed
c = moles of water formed
Now taking carbon balance on above reaction , we get
[ (0. 8062 CH4 + 0. 0541 C2H6 + 0. 0187 C3H8 + 0. 0160 C4H10 + 0. 1050 N2 ] + 2.8914 ( O2 + 3. 76 N2) ==>
12.931 (0. 078 C02 + 0. 002 C0 + 0. 07 O2 + 0. 85 N2) + 1.9295 H2O
Now Air- Fuel ration is given as
AF = ( moles of air ) / ( moles of fuel) = ( 2.8914) ( 1 + 3.76 ) / 1 = 13.763 kmol air / kmol fuel
B)
Now kmol fuel in 100 m3 of fuel at 300 K and 1 bar is calculated by ideal gas equation as
C)
For complete combustion of fuel reaction can be written as,
[ (0. 8062 CH4 + 0. 0541 C2H6 + 0. 0187 C3H8 + 0. 0160 C4H10 + 0. 1050 N2 ] + ( O2 + 3. 76 N2) ==>
C02 + N2 + H2O
Balancing this reaction we get,
[ (0. 8062 CH4 + 0. 0541 C2H6 + 0. 0187 C3H8 + 0. 0160 C4H10 + 0. 1050 N2 ] + 2.0 ( O2 + 3. 76 N2) ==>
1.0345 C02 + 7.625 N2 + 1.93 H2O
Now theoretical fuel-air ratio is given as
AF = ( moles of air ) / ( moles of fuel) = ( 2) ( 1 + 3.76 ) / 1 = 9.52 kmol air / kmol fuel
Percent theoretical air is given as
Percent theoretical air = ( ( Actual AF ratio ) / ( theoretical AF ratio ) ) * 100
= ( ( 13.763 kmol air / kmol fuel ) / ( 9.52 kmol air / kmol fuel ) ) * 100
Percent theoretical air = 144.56 %